As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) AT 1,500 HOUR INSPECTION, THE BOLT ATTACHING THE FLAP CONTROL CABLE TO THE BELLCRANK ARM WAS FOUND BENT APPROXIMATELY 9 DEGREES AT ITS MID-POINT. INSPECTION OF OPPOSITE BOLT ALSO FOUND BENT. IT IS SUSPECTED THAT THE BOLTS ARE BEING BENT WHEN THE FLAPS ARE SELECTED FULL DOWN WHERE THE AIR LOADS OF THE FLAP ARE TRANSMITTED ON EACH END OF THE SUBJECT BOLTS.